| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1967-059A  |
| SATCAT no. | 02842 |
| Mission duration | 217 days |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 400 kg[1] |
| Start of mission | |
| Launch date | 12 June 1967, 18:06:00 GMT |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk, Site 133/3 |
| Contractor | Yuzhnoye |
| End of mission | |
| Decay date | 15 January 1968 |
| Orbital parameters | |
| Reference system | Geocentric[2] |
| Regime | Low Earth |
| Perigee altitude | 198 km |
| Apogee altitude | 1515 km |
| Inclination | 81.9° |
| Period | 102.1 minutes |
| Epoch | 12 June 1967 |
Kosmos 165 (Russian: Космос 165 meaning Cosmos 165), also known as DS-P1-Yu No.11 was a radar calibration target satellite which was used by the Soviet Union for tests of anti-ballistic missiles. It was a 400 kilograms (880 lb) spacecraft,[1] which was built by the Yuzhnoye Design Office, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme.[3]
Kosmos 165 was launched using a Kosmos-2I 63SM carrier rocket, which flew from Site 133/3atPlesetsk Cosmodrome.[4] The launch occurred at 18:06:00 GMT on 12 June 1967.[5]
Kosmos 165 separated from its carrier rocket into a low Earth orbit with a perigee of 198 kilometres (123 mi), an apogee of 1,515 kilometres (941 mi), an inclination of 81.9°, and an orbital period of 102.1 minutes.[2]Itdecayed from orbit on 15 January 1968.[6] Kosmos 165 was the eighth of seventy nine DS-P1-Yu satellites to be launched,[3] and the seventh of seventy two to successfully reach orbit.[7]
This article incorporates text from this source, which is in the public domain.
This article incorporates text from this source, which is in the public domain.
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Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |
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